Path: Orbit/OrbitMechanics
% Computes the synodic period from semi-major axis. Type SynodicFromSemiMajorAxes for an example of Mars and Earth. -------------------------------------------------------------------------- Form: p = SynodicFromSemimajorAxes( a1, a2, mu ) -------------------------------------------------------------------------- ------ Inputs ------ al (1,1) Orbit 1 semi-major axis (km) a2 (1,1) Orbit 2 semi-major axis (km) mu (1,1) Gravitational constant ------- Outputs ------- p (1,1) Synodic period --------------------------------------------------------------------------
Orbit: OrbitMechanics/SynPer SC: BasicOrbit/Period Common: Database/Constant Common: Graphics/TimeLabl
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